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  • Internally damped, self-arresting vertical drop-weight apparatus [microform] / inventor, Damodar R. Ambur... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Formulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panels [microform] / Navin Jaunky and Norman F. Knight, Jr., Damodar R. Ambur.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Compression response of a sandwich fuselage keel panel with and without damage [microform] / David M. McGowan and Damodar R. Ambur.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Response of composite panels with stiffness gradients due to stiffener terminations and cutouts [microform] / Damodar R. Ambur ... [et al.].

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Damage characteristics and residual strength of composite sandwaich panels impacted with and without compression loading [microform] / : presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, session no. 15-damage tolerance : Long Beach, California, April 20-23, 1998 / David M. McGowan and Damodar R. Ambur.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Buckling analysis of anisotropic curved panels and shells with variable curvature [microform] / Navin Jaunky and Norman F. Knight, Jr.; Damodar R. Ambur.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets [microform] / David M. McGowan and Damodar R. Ambur.

    • Text
    • Hampton, Va. : Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS53733

  • Compression response of a sandwich fuselage keel panel with and without damage / David M. McGowan and Damodar R. Ambur.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 1997.
    • 1997-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS72357

  • Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets / David M. McGowan and Damodar R. Ambur.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 1997.
    • 1997-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS53733

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